General Electric YJ101
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| YJ101 | |
|---|---|
| Type | Turbofan |
| National origin | United States |
| Manufacturer | General Electric Aircraft Engines |
| First run | 1978 |
| Major applications | Northrop YF-17 |
| Developed into | General Electric F404 |
The General Electric YJ101 was an afterburning turbofan engine in the 15,000 lbf class (static thrust). Developed for the Northrop YF-17 entry in the Lightweight Fighter (LWF) competition, the YJ101 formed the basis for General Electric's highly successful F404 engine.
Contents
Applications
Specifications (YJ101)
General characteristics
- Type: Turbofan
- Length:
- Diameter:
- Dry weight:
Components
- Compressor: axial
- Combustors: annular
Performance
- Maximum power output:
- Power-to-weight ratio:
See also
- Related development
- Related lists
References
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External links
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